Patents by Inventor William B. Krueger
William B. Krueger has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 11768219Abstract: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.Type: GrantFiled: October 20, 2021Date of Patent: September 26, 2023Assignee: Rosemount Aerospace Inc.Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Patent number: 11649057Abstract: A static plate heating arrangement includes a faceplate including a port extending from an exterior surface of the faceplate to an interior surface of the faceplate, a fixed resistance heater in thermal communication with the interior surface and surrounding the port, and a self-regulating heater in thermal communication with the interior surface and surrounding the fixed resistance heater. The fixed resistance heater and the self-regulating heater are electrically connected in series.Type: GrantFiled: December 13, 2019Date of Patent: May 16, 2023Assignee: Rosemount Aerospace Inc.Inventors: Alexander N. Reid, Nathan Allan Hoffmann, William B. Krueger, Brian Alan Gilkison, Robert J. Johnson
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Publication number: 20230073840Abstract: An angle of attack sensor includes a housing having an open end and a closed end, a faceplate positioned on the open end of the housing, the faceplate comprising a periphery at an outer edge of the faceplate, a central opening, and an exterior surface extending from the periphery to the central opening, and a vane assembly extending through the central opening of the faceplate. The exterior surface of the faceplate has a sloped profile from the periphery to the central opening.Type: ApplicationFiled: February 25, 2021Publication date: March 9, 2023Inventors: Mackenzie Whalen, Aaron A. Cusher, Armando Valdes Chavez, Daniel Hanson, Richard Alan Schwartz, Wallace Johnson, William B. Krueger, Kaleb Anderson
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Publication number: 20220043022Abstract: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.Type: ApplicationFiled: October 20, 2021Publication date: February 10, 2022Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Patent number: 11181545Abstract: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.Type: GrantFiled: November 28, 2017Date of Patent: November 23, 2021Assignee: Rosemount Aerospace Inc.Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Publication number: 20210179277Abstract: A static plate heating arrangement includes a faceplate including a port extending from an exterior surface of the faceplate to an interior surface of the faceplate, a fixed resistance heater in thermal communication with the interior surface and surrounding the port, and a self-regulating heater in thermal communication with the interior surface and surrounding the fixed resistance heater. The fixed resistance heater and the self-regulating heater are electrically connected in series.Type: ApplicationFiled: December 13, 2019Publication date: June 17, 2021Inventors: Alexander N. Reid, Nathan Allan Hoffmann, William B. Krueger, Brian Alan Gilkison, Robert J. Johnson
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Patent number: 10730637Abstract: An angle of attack sensor includes a housing, a heated chassis positioned at least partially within the housing and defining a pocket, a mounting plate positioned adjacent the heated chassis and having a circular opening, an external surface facing away from the housing, and an internal surface facing toward the housing, and a vane assembly extending through the circular opening of the mounting plate. The vane assembly includes a vane extending from a root to a tip and a vane base connected to the root of the vane and positioned within the pocket of the heated chassis such that the vane base is offset inwardly from the external surface toward the housing.Type: GrantFiled: September 29, 2017Date of Patent: August 4, 2020Assignee: Rosemount Aerospace Inc.Inventors: William B. Krueger, Kenneth Freeman, Richard Alan Schwartz, Alexander N. Reid, Timothy DeAngelo
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Patent number: 10725065Abstract: An angle of attack sensor includes a vane that is freely rotatable to align with a direction of an oncoming airflow over the vane. The airfoil includes a root proximate a vane hub that connects to a rotatable shaft, a tip opposite the root, a leading edge, a trailing edge opposite the leading edge, a first lateral face, a second lateral face, and a heating element disposed within the airfoil between the first and second lateral faces proximate the leading edge. The first lateral face extends from the leading edge to the trailing edge. The second lateral face is opposite the first lateral face and extends from the leading edge to the trailing edge. The first and second lateral faces are symmetric about a chord of the airfoil and each have an outer surface profile that is nonlinear and geometrically convex from the leading edge to the trailing edge.Type: GrantFiled: November 14, 2016Date of Patent: July 28, 2020Assignee: Rosemount Aerospace Inc.Inventors: William B. Krueger, Alexander N. Reid, Richard Alan Schwartz, Kenneth Freeman
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Patent number: 10457412Abstract: The bearings of aircraft angle of attack (AOA) vanes are susceptible to lightning strike damage, which causes fluting on the inner and outer races of the bearings and causes the bearings to generate friction, noise, and vibrations. To prevent the bearings from experiencing damage due to lightning strikes, the bearings, the shaft, and/or the mounting plate are configured to create an electric isolator to prevent the electric current from the lightning strike from passing through the bearings, thereby preventing the bearings from incurring lightning strike damage.Type: GrantFiled: September 16, 2016Date of Patent: October 29, 2019Assignee: Rosemount Aerospace Inc.Inventors: William B. Krueger, Richard Alan Schwartz, Kenneth Freeman
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Patent number: 10393766Abstract: An angle of attack sensor includes a housing having an open first end and a closed second end, a heated chassis positioned within the open first end of the housing, a mounting plate positioned on the heated chassis adjacent the open first end of the housing such that an internal chamber is formed between the heated chassis and the mounting plate, a transducer compartment between the heated chassis and the closed second end of the housing, and a water management system located adjacent the internal chamber and the transducer compartment. The water management system includes an annular chamber positioned in the internal chamber, a first tube at a first end of the annular chamber, and a second tube at a second end of the annular chamber. The first tube has a hole such that the first tube is in fluid communication with the annular chamber and the internal chamber, and the second tube is in fluid communication with the annular chamber and the transducer compartment.Type: GrantFiled: August 17, 2017Date of Patent: August 27, 2019Assignee: Rosemount Aerospace Inc.Inventors: Carlos Alcaya, Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Publication number: 20190100327Abstract: An angle of attack sensor includes a housing, a heated chassis positioned at least partially within the housing and defining a pocket, a mounting plate positioned adjacent the heated chassis and having a circular opening, an external surface facing away from the housing, and an internal surface facing toward the housing, and a vane assembly extending through the circular opening of the mounting plate. The vane assembly includes a vane extending from a root to a tip and a vane base connected to the root of the vane and positioned within the pocket of the heated chassis such that the vane base is offset inwardly from the external surface toward the housing.Type: ApplicationFiled: September 29, 2017Publication date: April 4, 2019Inventors: William B. Krueger, Kenneth Freeman, Richard Alan Schwartz, Alexander N. Reid, Timothy DeAngelo
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Publication number: 20190104568Abstract: A heating system includes a voltage source, a heating circuit, and a current sensor. The voltage source is configured to provide a current. The heater circuit is electrically coupled to the voltage source. The heater circuit includes a heater array and a compensation circuit. The heater array is configured to provide heat to a region using the current. The compensation circuit is electrically coupled to the voltage source in parallel with the heater array. The compensation circuit is configured to maintain the current above a threshold current level when the heater array is operable. The current sensor is configured to measure a level of the current to the heater circuit and output an alert in response to the current falling below the threshold current level.Type: ApplicationFiled: September 29, 2017Publication date: April 4, 2019Inventor: William B. Krueger
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Publication number: 20190056424Abstract: An angle of attack sensor includes a housing having an open first end and a closed second end, a heated chassis positioned within the open first end of the housing, a mounting plate positioned on the heated chassis adjacent the open first end of the housing such that an internal chamber is formed between the heated chassis and the mounting plate, a transducer compartment between the heated chassis and the closed second end of the housing, and a water management system located adjacent the internal chamber and the transducer compartment. The water management system includes an annular chamber positioned in the internal chamber, a first tube at a first end of the annular chamber, and a second tube at a second end of the annular chamber. The first tube has a hole such that the first tube is in fluid communication with the annular chamber and the internal chamber, and the second tube is in fluid communication with the annular chamber and the transducer compartment.Type: ApplicationFiled: August 17, 2017Publication date: February 21, 2019Inventors: Carlos Alcaya, Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Publication number: 20190056425Abstract: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.Type: ApplicationFiled: November 28, 2017Publication date: February 21, 2019Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Publication number: 20180136249Abstract: An angle of attack sensor includes a vane that is freely rotatable to align with a direction of an oncoming airflow over the vane. The airfoil includes a root proximate a vane hub that connects to a rotatable shaft, a tip opposite the root, a leading edge, a trailing edge opposite the leading edge, a first lateral face, a second lateral face, and a heating element disposed within the airfoil between the first and second lateral faces proximate the leading edge. The first lateral face extends from the leading edge to the trailing edge. The second lateral face is opposite the first lateral face and extends from the leading edge to the trailing edge. The first and second lateral faces are symmetric about a chord of the airfoil and each have an outer surface profile that is nonlinear and geometrically convex from the leading edge to the trailing edge.Type: ApplicationFiled: November 14, 2016Publication date: May 17, 2018Inventors: William B. Krueger, Alexander N. Reid, Richard Alan Schwartz, Kenneth Freeman
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Publication number: 20180079525Abstract: The bearings of aircraft angle of attack (AOA) vanes are susceptible to lightning strike damage, which causes fluting on the inner and outer races of the bearings and causes the bearings to generate friction, noise, and vibrations. To prevent the bearings from experiencing damage due to lightning strikes, the bearings, the shaft, and/or the mounting plate are configured to create an electric isolator to prevent the electric current from the lightning strike from passing through the bearings, thereby preventing the bearings from incurring lightning strike damage.Type: ApplicationFiled: September 16, 2016Publication date: March 22, 2018Inventors: William B. Krueger, Richard Alan Schwartz, Kenneth Freeman
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Patent number: 7497123Abstract: A direct mount for coupling a pressure transmitter to a process fluid of an industrial process includes a transmitter coupling configured to couple to a pressure transmitter. A process coupling is configured to couple an industrial process. A capillary tube extends between the transmitter coupling and the process coupling. A thermally conductive path having relatively high thermal conductivity extends between the process coupling and the transmitter coupling. Preferably, a thermal switch selectively thermally connects the thermally conductive path between the process coupling and the transmitter coupling.Type: GrantFiled: December 18, 2007Date of Patent: March 3, 2009Assignee: Rosemount Inc.Inventors: Steven M. Behm, William B. Krueger, Jay W. Smith, Jeffrey P. Reddick, Jeffrey Graupmann, Aaron Seelig
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Patent number: 6510740Abstract: A pressure transmitter with a transmitter housing having an outer wall providing thermal resistance. The outer wall extends from an isothermal island at a first end to a heat sink island at a second end. The isothermal island includes a fluid inlet, and pressure and temperature sensors. The heat sink island includes a primary heat load device that is heat sunk to an outer shell of an electrical connector. The connector contacts carry a current controlled by the transmitter, and a portion of the current is conducted by a primary heat load device. A circuit board controls the current to represent the pressure. A high accuracy, temperature compensated current output represents pressure.Type: GrantFiled: September 21, 2000Date of Patent: January 28, 2003Assignee: Rosemount Inc.Inventors: Steven M. Behm, William B. Krueger, Kelly M. Orth, Jeffrey C. Brekken
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Patent number: 6059254Abstract: A process instrument mount includes an outer wall and an inner wall. The outer wall is separated from the inner wall by a space. The mount has a first end and a second end, and a hole extends from the first end to the second end. The inner wall surrounds the hole, and has a threaded region to receive a process instrument from the first end. The inner wall also has a flange proximate the second end to sealingly mate with the process instrument. In one embodiment the inner and outer walls are portions of a unitary metal block, and the space separating them comprises a groove formed in the metal. In another embodiment the inner and outer walls are separate parts joined together at the second end and spaced apart between the first and second ends.Type: GrantFiled: March 27, 1997Date of Patent: May 9, 2000Assignee: Rosemount Inc.Inventors: Paul C. Sundet, William B. Krueger
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Patent number: 5333504Abstract: A low range pressure sensor includes a base plate of brittle material, and a diaphragm plate mounted on the base plate and sealed around a periphery to the base plate. Pressures are introduced to cause the diaphragm to deflect toward the base plate, and the deflection of the diaphragm is sensed through strain gauges to provide an indication of the pressure. The diaphragm is provided with a plurality of individual support posts on a side facing the base plate, so that when the diaphragm is deflected toward the base plate under high overpressures the support posts will support the diaphragm against movement to avoid failure or breakage of the diaphragm. The number of support posts can be varied as desired.Type: GrantFiled: September 1, 1992Date of Patent: August 2, 1994Assignee: Rosemount Inc.Inventors: Mark A. Lutz, William B. Krueger